BACKGROUND OF THE INVENTION
1. Field of the Invention
[0001] The present invention relates to protective materials and, more specifically, to
a material that diminishes the effect of a shock wave.
2. Description of the Related Art
[0002] Material designs for handling the impact of an external stimulus, such as a blast,
as shock wave or projectiles, include, for example, woven fabrics, ceramic materials,
and composite systems. Kevlar®, Zylon®, Armos®, Spectra® are commercially available
fabrics made from high-strength fibers. Another material is ballistic steel, which
is comprised of hardened high tensile steel, woven into fiber form. Further, boron
carbide can be used as a material, for example, in the production of body armor.
[0003] Ceramic materials, in particular ceramic metal composites have found utility in light
weight body armor.
[0004] Existing systems attempt to attenuate shock waves by presenting a high mass material
between the source of the shock wave and the thing being protected. The high mass
material absorbs some of the shock wave energy, thereby resulting in a shock wave
of decreased amplitude. However, while the wave's amplitude may be decreased, it is
only decreased by a certain amount and may still do considerable damage.
[0005] Therefore, there is a need for a material that disrupts a shock wave, thereby lessening
its effect.
[0007] WO 2010/019609 A1 discloses engineered composite materials suitable for applications that can benefit
from a composite material capable of interacting with or responding to, in a controlled
or predetermined manner, changes in its surrounding environment. The composite material
generally includes a gradient layer structure of a sequence of at, e.g., three or
more gradient-contributing layers of microscale particles, wherein a mean particle
size of particles of neighboring gradient-contributing layers in the cross section
of the gradient layer structure varies from layer to layer, thereby forming a particle
size gradient, and in contact with the gradient layer structure, a densely packed
particle structure including densely packed microscale particles, wherein a mean particle
size of the densely packed microscale particles does not form a particle size gradient
in the cross section of the densely packed particle structure.
[0008] WO 03/025493 A1 discloses a structure arrangement and method for the protection of a host system
against an impacting ballistic element. The structure arrangement includes a composite.
The composite includes a matrix and a multiplicity of single-walled carbon nanotubes.
The single-walled carbon nanotubes are arranged with respect to the matrix so as to
define an array for engagement with an impacting ballistic element.
SUMMARY OF THE INVENTION
[0009] The present invention is a shock wave attenuating material as defined in Claim 1
of the appended claims. Some embodiments of the invention are set out in the dependent
claims.
[0010] The disadvantages of the prior art are overcome by the present invention which, in
one embodiment, provides a shock wave attenuating material that includes a substrate
layer. A plurality of shock attenuating layers is disposed on the substrate layer.
Each of the plurality of shock attenuating layers includes a gradient nanoparticle
layer including a plurality of nanoparticles of different diameters that are arranged
in a gradient from smallest diameter to largest diameter and a graphitic layer disposed
adjacent to the gradient nanoparticle layer. The graphitic layer includes a plurality
of carbon allotrope members suspended in a matrix.
[0011] Another embodiment of the invention provides a helmet that includes a helmet member
configured to be worn by a user. A plurality of shock attenuating layers is applied
to the helmet member. Each shock attenuating layer includes a gradient nanoparticle
layer including a plurality of nanoparticles of different diameters that are arranged
in a gradient from smallest diameter to largest diameter; and a graphitic layer disposed
adjacent to the gradient nanoparticle layer, the graphitic layer including a plurality
of carbon allotrope members suspended in a matrix.
[0012] Another embodiment of the invention provides an armor unit that includes a structural
element, an armor plate and a plurality of shock attenuating layers. The plurality
of shock attenuating layers is disposed in a predetermined relationship with at least
one of the structural element and the armor plate. Each shock attenuating layer includes
a gradient nanoparticle layer including a plurality of nanoparticles of different
diameters that are arranged in a gradient from smallest diameter to largest diameter;
and a graphitic layer disposed adjacent to the gradient nanoparticle layer, the graphitic
layer including a plurality of carbon allotrope members suspended in a matrix.
[0013] Yet another embodiment of the invention provides a personal body armor unit that
includes a ceramic plate, a high mass member and a nanoparticle shock wave attenuating
material layer. The high mass member is disposed adjacent to the ceramic plate. The
nanoparticle shock wave attenuating material layer is disposed on the high mass member.
[0014] The nanoparticle shock wave attenuating material layer can be disposed between the
high mass member and the ceramic plate. Similarly, the nanoparticle shock wave attenuating
material layer can be disposed outside of the high mass member or the ceramic plate
or both. It is understood that any combination of these configurations fall within
the scope of the invention.
[0015] These and other aspects of the invention will become apparent from the following
description of the preferred embodiments taken in conjunction with the following drawings.
As would be obvious to one skilled in the art, many variations and modifications of
the invention may be effected without departing from the scope of the appended claims.
BRIEF DESCRIPTION OF THE FIGURES OF THE DRAWINGS
[0016]
FIG. 1 is a schematic diagram of one embodiment of a shock wave attenuating material.
FIG. 2A is a schematic diagram of one embodiment of a gradient nanoparticle layer.
FIG. 2B is a schematic diagram of one embodiment of a graphitic layer.
FIG. 3 is a schematic diagram of the embodiment shown in FIG. 1, demonstrating shock wave
attenuation.
FIG. 4 is a schematic diagram of one embodiment of a helmet.
FIG. 5 is a schematic diagram of one embodiment of an armor unit.
FIG. 6 is a schematic diagram of one embodiment of a body armor unit.
FIG. 7 is a schematic diagram of one embodiment of a body armor unit.
FIG. 8 is a schematic diagram of one embodiment of a body armor unit.
DETAILED DESCRIPTION OF THE INVENTION
[0017] A preferred embodiment of the invention is now described in detail. Referring to
the drawings, like numbers indicate like parts throughout the views. Unless otherwise
specifically indicated in the disclosure that follows, the drawings are not necessarily
drawn to scale. As used in the description herein and throughout the claims, the following
terms take the meanings explicitly associated herein, unless the context clearly dictates
otherwise: the meaning of "a," "an," and "the" includes plural reference, the meaning
of "in" includes "in" and "on."
[0018] U.S Patent Application No.
12/672,865 (Publication No.
US 2011/0212320 A1) discloses a gradient nanoparticle composite material and a method of making a gradient
nanoparticle composite material.
[0019] As shown in FIG. 1, one embodiment of a shock wave attenuating material
100 includes a substrate layer
104 and a plurality
110 of shock attenuating layers disposed on the substrate layer. Each of the plurality
110 of shock attenuating layers includes a gradient nanoparticle layer
114 and a graphitic layer
118 disposed adjacent to the gradient nanoparticle layer
114. In a typical embodiment, the shock wave attenuating material
100 would include at least 10 gradient nanoparticle layers
114 alternating with at least 10 graphitic layers
118 (while only three are shown in FIG. 1 for the sake of simplicity).
[0020] As shown in FIG. 2A, each nanoparticle layer
114 includes a plurality of nanoparticles
120 of different diameters (at least two different diameters) that are arranged in a
gradient from smallest diameter to largest diameter. The specific orientation of the
gradient (smallest to largest vs. largest to smallest) depends on the specific application
for which the material is being used.
[0021] As shown in FIG. 2B, the graphitic layer
118 includes a plurality of carbon allotrope members
128 suspended in a matrix
124. The carbon allotrope members
128 can include graphene sheets, carbon nanotubes, fullerenes, functionalized graphene
sheets, functionalized carbon nanotubes, and functionalized fullerenes.
[0022] Depending upon any transparency requirement, the nature of the substrate may be varied.
Two potential substrates are polycarbonate and carbon fiber composites/laminates.
In fact, a thicker (yet still transparent) polymer-graphene composite layer may be
employed directly as the substrate. The gradient structure may be any of those shown,
for example, in U.S. Patent Publication No.
US-2011-0212320-A1, as well as others built up from the same principles. One embodiment of a gradient
structure has a total thicknesses of the order of 5-10µm, which can then be repeated
as many times as required.
[0023] A fullerene layer may be directly deposited by coating, from a toluene solution,
onto the gradient structure in thicknesses as small as a monolayer. Similarly, nanotubes
and graphene or graphene oxide sheets may be coated from suspensions in organic solvents
such as chloroform. However, these two allotropes may also be (preferentially) deposited
as polymer composites. The use of a polymer composite provides additional structural
integrity to the overall coating and, more importantly, provides additional impact
regions for the generation of partially reflected shock waves and will further reduce
the overall passage of the shock energy from the impact site to the protection site.
Carbon allotrope members
128 can be functionalized as a graphene oxide. Similarly, nanotubes and fullerenes can
be functionalized with carboxylic acid, amines, can be hydroxylated or carboxylated.
[0024] As shown in FIG. 3, the graphitic layers
118 are of a thickness that is sufficient to reflect at least a portion of a shock wave
impinging thereon. The thickness of the graphitic layers
118 will depend on the type of shock wave that the designer desires to protect against.
When a shock wave
302 impinges on the material
100, the first gradient nanoparticle layer
114 begins to attenuate the shock wave
304 and the first graphitic layer
118 reflects a portion of the shock wave
306, thereby generating destructive interference with any residual shock wave energy.
Successive waves
308 and
312 reflect in a similar fashion to generate reflected waves
310 and
314, which further interfere with residual shock energy.
[0025] The carbon or carbon composite layers mark the end of one nanostructure and the start
of the next. A significant reduction of the incident shock wave occurs after passage
through less than 10µm of gradient nanoparticles. Stacks or layers of such structures
with the carbon and/or carbon composites are interspersed and define the layer or
stack limit. The effect, at each carbon interface, will be to create a backward traveling
wave causing attenuation of the incident shock wave, as well as a much reduced forward
transmitted shock wave, which passes into the next layer of the structure. A stack
of 50 alternating gradient nanoparticle structures (each composed of 30 nanoparticle
layers) and composite layers would result in a 1 mm thick coating and significant
attenuation of the incident shock wave. Each of these 50 gradient or composite layers
is one-fifth the thickness of the typical human hair.
[0026] As shown in FIG. 4, the shock wave attenuating material
110 can be part of a helmet
400 or helmet liner. In one embodiment, a helmet
400 includes a helmet member
402 configured to be worn by a user, such as an Enhanced Combat Helmet [ECH] used in
military applications. The helmet member
402 could be made from a para-aramid synthetic fiber composite, such as Kevlar
®. In other embodiments, the helmet could be of the type used in sports. For example,
the shock wave attenuating material
110 could be used in a baseball helmet, a football helmet, a hockey helmet, a bicycling
helmet, or the like. The helmet
400 could include an outer shell (such as, e.g., acrylonitrile butadiene styrene), a
shock wave attenuating material
110 layer and an inner shell. The helmet
400 could even include an outer shell and several layers of shock wave attenuating material
110 alternating with high mass material layers. The high mass material could include,
for example, a high density plastic, a composite, fiberglass, a para-aramid synthetic
fiber composite, a vinyl, acrylonitrile butadiene styrene, an acrylic, a metal, or
any other material typically used in a helmet. A shock-absorbing foam liner may also
be added to the helmet.
[0027] As shown in FIG. 5, the shock wave attenuating material
110 can be part of an armor unit
500, which can include a structural element
502, such as a vehicle panel. An outer armor plate
510, such as a ceramic or composite plate, provides an outer armor surface. The shock
wave attenuating material
110 is disposed between the structural element
502 and the armor plate
510. The shock wave attenuating material
110 could also be outside of either the structural element
502 or the armor plate
510 or both. It will be appreciated that any combination of these configurations will
fall within the scope of the invention.
[0028] As shown in FIG. 6, one embodiment is a body armor assemblage
600, such as an interceptor body armor assemblage (of the type used in the Improved Outer
Tactical Vest, Improved Modular Tactical Vest and the US Army and USMC plate carriers).
Such an assemblage
600 would include an armor plate
602 (such as a ceramic plate) with a high mass member. Examples of materials suitable
for use in the high mass member include: a high density polymer
610 (such as an ultra high molecular weight polyethylene), a para-aramid synthetic fiber
composite, a carbon fiber composite, a metal, a ceramic and combinations thereof.
The shock wave attenuating material
110 can be applied to the high density polymer
610 on the high density polymer
610 opposite from the armor plate
602 on the side adjacent to the body of the user. This latter application helps solve
the problem of backface deformation. As shown in FIG. 7, in one embodiment of a personal
body armor assemblage
620, the shock wave attenuating material
110 is disposed between the high density polymer
610 and the armor plate
602. As shown in FIG. 8, multiple layers of shock wave attenuating material
110 may be applied to the armor assemblage
630.
[0029] In one application, the shock wave attenuating material
110 can be applied to such devices as soccer shin guards, baseball catcher's chest pads,
football shoulder pads, baseball mitts and the like. It can also be applied to such
devices as golf clubs and baseball bats to reduce the effects of shock associated
with their use.
[0030] In some embodiments, the gradient nanoparticle composite material is capable of absorbing
an impact of a shock wave that, for example, is produced by an explosion or caused
during operation of a device. In some embodiments, the gradient nanoparticle composite
material is capable of mitigating and/or remediating one or more secondary blast effects
resulting from the explosion.
[0031] In some embodiments, the gradient nanoparticle composite material is capable of reacting
to and/or interacting with one or more stimuli existing in a blast zone environment.
For example, in some embodiments the material can absorb at least a portion of an
initial blast impact and/or the overpressure wave resulting from an explosion. In
addition, or alternatively, gradient nanoparticle composite material can be designed
to mitigate and/or remediate one or more related blast effects resulting from the
blast impact itself. Thus, some embodiments can provide a composite material that
through intelligent design of the system can not only reduce blast impact with greater
efficiency and efficacy, but that can also mitigate and/or remediate one or more secondary
blast effects.
[0032] In some embodiments, the gradient nanoparticle composite material can provide bomb
blast mitigation and/or remediation by reducing the reflective value of the bomb blast
by absorption of the bomb blast energy. In some embodiments, the primary mitigating
and/or remediating process can be by absorption of the bomb blast shock wave. In some
embodiments, the mitigating and/or remediating process can be by absorption of the
pre-overpressure wave that precedes the shock wave. Absorption of the shock wave and/or
the pre-overpressure wave can occur through one or more mechanisms, including, for
example, momentum transfer, destruction of the spatial symmetry of, e.g., the blast
wave, plastic deformation, rupture of particles, e.g. filled and unfilled core-shell
particles, restitution, and interparticle/interlayer shear.
[0033] In some embodiments, the gradient nanoparticle composite material can provide a platform
from which a wide variety of blast effects can be mitigated and/or remediated. For
example, in a filled-shell material the absorbed energy can be utilized to rupture,
e.g., microcapsules to introduce a series or selection of materials or material systems
into the blast environment and to thus mitigate and/or remediate the blast effects.
In some embodiments, the gradient nanoparticle composite material can provide a relatively
light weight material that can be applied to pre-existing structures or systems with
no deleterious effects on the performance attributes of the pre-existing structure
or system.
[0034] Some embodiments provide bomb proofing, impact or smart material applications. Examples
of bomb proof applications include receptacles and liners (such as in waste receptacles
and bags etc.), satellites, helicopters, and high tech devices (computer/hardware
casings, cable protection), construction (buildings and their facades), bridges and
their structural members, pipes and pipelines (for fossil fuels, conduits, utilities),
automotive (door panels, bumpers, dashboards, windshields and windows, undercarriages
and roofs), aerospace (interior/exterior of planes), etc. In some embodiments, the
gradient nanoparticle composite material can be used in connection with military equipment,
structures, vehicles, vessels and crafts for land, sea, and airborne forces to include
armored and unarmored vehicles, aircraft, (which includes helicopters and unmanned
drones), and nautical vessels such as submarines, ships, boats and the like.
[0035] For military and civilian uses, the gradient nanoparticle composite material can
be applied as an exterior coating, film, intermediate layer and/or as a panel to pre-existing
equipment or, alternatively, can be utilized for forming structural components of
the military vehicle, aircraft, or nautical vessel.
[0036] The application of gradient nanostructured composites for the attenuation of shock
waves is based on the same principles that apply macroscopic granular spheres to create
blast walls. Granular materials, especially arranged in a gradient, create mismatching
of the solitary wave at each particle contact point and, hence, attenuation of that
wave. The effect is a combination of passive and active physical processes: absorption,
distortion, and engineered redirection of the shock wave without appreciable heating.
In effect, the composite causes destructive interference of the shock wave to attenuate
the incident wave. The composite, an ordered structure including selected solid, hollow
and filled nanoparticles, may be coated onto a surface (e.g., a protective device,
such as a helmet) and may also be produced as a self-supported liner (using plastic
containment). Additionally, while the gradient array provides shock attenuation, the
material within the filled nanoparticles acts to create an indicator that the user
has experienced a shock wave sufficient to cause mild or severe traumatic brain injury
while wearing the protective device, such as a helmet. The final product is a lightweight
coating that does not change the flexibility of the treated material and which can
be made transparent by careful choice of nanoparticle materials. After activation,
the protective device may be recoated, if that technology was used in production,
or the liner may be replaced, if that approach was employed.
[0037] One-dimensional models of a shock wave propagating through a homogeneous or a tapered
granular chain demonstrate shock wave attenuation. While three-dimensional structures
are too complex for existing modeling systems, the major properties observed for one
dimensional calculations are valid in the three-dimensional case. Assuming no elastic
effects and no loading, the spheres are simply touching at a single point of contact,
the kinetic energy loss is calculated as a function of the change in sphere radius,
q, as a wave travels through the spheres, the energy lost per collision in the spheres,
E
L, and the number of spheres, N, in the chain:

The values of
q and
N are fixed by the experiment; the loss term is defined by the ratio of the loading
force as two particles come together under the influence of a wave and the unloading
forces, as they separate. The decrease in kinetic energy predicted by Equation (1),
KE
OUT/KE
IN, is independent of the size of the spheres. The decrease in kinetic energy occurs
because each particle absorbs some of the incident energy and that energy remains
with the particle. Note that for small values of
N, a chain of constant size (
q = 0) exhibits little loss of kinetic energy. For values of
q of the order of 10% and elastic losses of approximately 5%, as much as 80% of the
input energy may be absorbed in a chain of 20 spheres. Experimental evidence confirms
the theoretical prediction. The large number of nanoparticles in a typical coating
provides a large number of the particle to particle contact points required by Equation
(1) and also serves to dissipate the kinetic energy surrendered by the incident shock
wave without appreciable heating of the coating.
[0038] Experimental evidence and theory indicate that the concept and its shock attenuation
benefit are independent of particle size. That fact opens the door to using the principles
to design nanostructures with a tapered chain-like structure. Such a structure is
inherently three-dimensional and beyond the current theoretical models. However, careful
consideration indicates that it is best described as a gradient
array of nanoparticles; a structure tapered in multiple directions and offering increased
attenuation of incoming shock waves. The structure could be built from monolayers
of nanoparticles deposited on a substrate beginning with the smallest radius and growing
larger with a
q of approximately 10%, the monolayer gradient could be reversed, either gradient could
be repeated in order or alternating gradients that reverse the order of the nanoparticle
layers could be constructed or multiple layers of each particle size could be used
to construct the gradient. Moreover, chemically modified nanoparticles present the
opportunity to add functionality to the nanostructure. The nanospheres may be solid
and made of any number of polymers, metals, ceramics or other materials, so that the
elastic properties and the interparticle forces may be varied. Hollow nanoparticles
offer an interesting capability to insert voids, spheres shattered under compression
by the shock wave, which would only act when the particles are compressed by sufficient
force. Polymer nanoparticle shells may be constructed to carry other materials within
the nanoparticle, providing the means to include in the structure indicators of the
passage of a blast wave or the ability to release a beneficial agent to the users
upon activation by the blast wave. The final product is a lightweight coating that
does not change the flexibility of the treated material and can be made transparent
by careful choice of nanoparticle materials. Taken as a whole, these characteristics
of nanostructured gradient arrays provide a menu for the development of blast wave
protection with targeted applications.
[0039] One version involves a structure that incorporates carbon allotrope (fullerene, nanotubes
or graphene) and/or carbon allotrope-polymer composite layers into the overall structure.
The carbon allotropes provide increased strength to the nanostructure since these
materials rank among the strongest known. One embodiment employs "stacks" or "layers"
of such structures with the carbon and/or carbon composites interspersed and defining
the layer or stack limit. The effect, at each carbon interface, is to create a backward
traveling wave causing attenuation of the incident shock wave, as well as a greatly
reduced forward transmitted shock wave, which passes into the next layer of the structure.
A stack of 50 gradient nanoparticle structures (each composed of 30 nanoparticle layers)
and composite layers would result in a 1mm thick coating and significant attenuation
of the incident shock wave. This structure would have a thickness of approximately
100 µm or 10 human hairs.
[0040] In one experimental embodiment, samples were made using a spin coating technique
and measuring approximately 6 cm
2. Samples having a wide variety of gradients and employed solid polymer, solid silica,
hollow polymer and filled (with long-chain hydrocarbons, as prototypes) silica nanoparticles
were employed. Mono-dispersed coatings, tapered gradients (large to small and small
to large) and repetitive gradients using polycarbonate substrates treated with UV
light to make the surface polar were also used. Most samples employed a hexagonal
close packing of the nanoparticles. The coatings typically had a tapered gradient
of 320nm/ 260nm/ 220nm/ 160nm/ 130nm. A laboratory-built impact tester was used to
explore the effects of the nanostructures on the shock wave caused by the impact of
a falling mass. The maximum in the impact shock wave was reduced in magnitude and
delayed relative to initiation of the event. The reduced force was also spread over
a greater temporal region to minimize the net effect. A list of some of our results
is contained in the table below, along with brief descriptions of the nanosphere gradients.
[0041] The following table shows experimental impact shock results for polystyrene or silica
nanospheres between two treated polycarbonate plates. The nanoparticles were solid
spheres, except the 400nm size, which were hollow:
| Sample |
Max. Force, N |
Width, ms |
Delay, ms |
Comments |
| Bare sensor |
1334 |
0.16 |
-- |
Control-no sample at all |
| Polycarbonate x2 |
1156 |
0.27 |
0.10 |
Control-two polycarbonate substrates |
| #1 |
872 |
0.31 |
0.18 |
130-160-220-260: 8 repeats/4 layers |
| #3 |
783 |
0.30 |
0.21 |
130-160-220-260-220-160: 5 repeats/6 layers |
| #5 |
623 |
0.34 |
0.22 |
130-160-220-260-320-400-320-260-220-160: 3 repeats/10 layers |
| #7 |
712 |
0.31 |
0.20 |
150-150-150 (silica): 30 repeats/1 layer |
| #8 |
578 |
0.34 |
0.24 |
320-400:13 repeats/2 layers |
| #10 |
712 |
0.30 |
0.21 |
400-320-260-220-160-130:4 repeats/6 layers |
[0042] The above described embodiments, while including the preferred embodiment and the
best mode of the invention known to the inventor at the time of filing, are given
as illustrative examples only. It will be readily appreciated that many deviations
may be made from the specific embodiments disclosed in this specification without
departing from the scope of the invention as defined in the appended claims. Accordingly,
the scope of the invention is to be determined by the claims below rather than being
limited to the specifically described embodiments above.
1. A shock wave attenuating material (100), comprising:
a plurality of shock attenuating layers (110), each including:
(i) a gradient nanoparticle layer (114) including a plurality of nanoparticles (120)
of different diameters that are arranged in a gradient; and
(ii) a carbon allotrope layer (118) disposed adjacent to the gradient nanoparticle
layer (114), the carbon allotrope layer (118) including a plurality of carbon allotrope
members (128) suspended in a matrix (124).
2. The shock wave attenuating material of Claim 1, wherein the gradient nanoparticle
layer (114) comprises nanoparticles (120) of at least two different diameters.
3. The shock wave attenuating material of Claim 1, wherein the carbon allotrope members
(128) are selected from a list of carbon allotropes consisting of: graphene sheets,
carbon nanotubes, fullerenes, functionalized graphene sheets, functionalized carbon
nanotubes, functionalized fullerenes and combinations thereof.
4. The shock wave attenuating material of Claim 1, further comprising a substrate layer
(104), wherein the plurality of shock attenuating layers (110) are disposed on the
substrate layer (104).
5. The shock wave attenuating material of Claim 1, wherein the gradient comprises the
plurality of nanoparticles (120) of different diameters arranged in a gradient array
from smallest diameter to largest diameter.
6. A helmet (400) or helmet liner comprising the shock wave attenuating material of Claim
1.
7. The helmet (400) of Claim 6, further comprising a material selected from the group
consisting of: a high density plastic, a composite, fiberglass, a para-aramid synthetic
fiber composite, a vinyl, acrylonitrile butadiene styrene, an acrylic, a metal.
8. An armor unit (500) comprising the shock wave attenuating material of Claim 1, wherein
the armor unit (500) further comprises a structural element (502) and an armor plate
(510).
9. The armor unit (500) of Claim 8, wherein the structural element (502) comprises at
least one of a ceiling, a floor or a wall of a vehicle.
10. The armor unit (500) of Claim 8, wherein the structural element (502) comprises a
body armor assemblage.
11. A personal body armor unit (600) comprising a ceramic plate (602), a high mass member
(610), and the shock wave attenuating material of Claim 1 disposed on the high mass
member.
12. The personal body armor unit (600) of Claim 11, wherein the high mass member (610)
comprises a material selected from a list of materials consisting of: ultra high molecular
weight polyethylene, a para-aramid synthetic fiber composite, a carbon fiber composite,
a metal, a ceramic and combinations thereof.
13. A computer or hardware casing comprising the shock wave attenuating material of Claim
1.
14. An exterior coating, film, intermediate layer and/or panel comprising the shock wave
attenuating material of Claim 1, applied to pre-existing equipment.
15. A soccer shin guard, baseball catcher's chest pad, football shoulder pad, baseball
mitt, golf club or baseball bat comprising the shock wave attenuating material of
Claim 1.
1. Schockwellen-Dämpfungsmaterial (100), umfassend:
eine Vielzahl von Schockdämpfungsschichten (110), die jeweils Folgendes einschließen:
(i) eine Gradienten-Nanopartikelschicht (114), die eine Vielzahl von Nanopartikeln
(120) mit verschiedenen Durchmessern einschließt, die in einem Gradienten angeordnet
sind; und
(ii) eine Kohlenstoffallotropschicht (118), die unmittelbar benachbart zu der Gradienten-Nanopartikelschicht
(114) abgelagert ist, wobei die Kohlenstoffallotropschicht (118) eine Vielzahl von
Kohlenstoffallotropgliedern (128) in einer Matrix (124) suspendiert einschließt.
2. Schockwellen-Dämpfungsmaterial nach Anspruch 1, wobei die Gradienten-Nanopartikelschicht
(114) Nanopartikel (120) mit mindestens zwei verschiedenen Durchmessern umfasst.
3. Schockwellen-Dämpfungsmaterial nach Anspruch 1, wobei die Kohlenstoffallotropglieder
(128) aus einer Liste von Kohlenstoffallotropen ausgewählt sind, bestehend aus:
Graphenfolien, Kohlenstoffnanoröhren, Fullerenen,
funktionalisierten Graphenfolien, funktionalisierten Kohlenstoffnanoröhren, funktionalisierten
Fullerenen und Kombinationen davon.
4. Schockwellen-Dämpfungsmaterial nach Anspruch 1, weiter umfassend eine Substratschicht
(104), wobei die Vielzahl von Schockdämpfungsschichten (110) auf der Substratschicht
(104) abgelagert sind.
5. Schockwellen-Dämpfungsmaterial nach Anspruch 1, wobei der Gradient die Vielzahl von
Nanopartikeln (120) mit verschiedenen Durchmessern umfasst, die in einem Gradienten-Array
vom kleinsten Durchmesser bis zum größten Durchmesser angeordnet sind.
6. Helm (400) oder Helmfutter, umfassend das Schockwellen-Dämpfungsmaterial nach Anspruch
1.
7. Helm (400) nach Anspruch 6, weiter umfassend ein Material, das aus der Gruppe ausgewählt
ist, bestehend aus:
einem Kunststoff hoher Dichte, einem Verbundstoff, Glasfasern, einem synthetischen
para-Aramid-Faserverbundstoff, einem Vinyl, Acrylnitril-Butadien-Styrol, einem Acryl,
einem Metall.
8. Panzerungseinheit (500), umfassend das Schockwellen-Dämpfungsmaterial nach Anspruch
1, wobei die Panzerungseinheit (500) weiter ein Strukturelement (502) und eine Panzerungsplatte
(510) umfasst.
9. Panzerungseinheit (500) nach Anspruch 8, wobei das Strukturelement (502) mindestens
eines von einer Decke, einem Boden oder einer Wand eines Fahrzeugs umfasst.
10. Panzerungseinheit (500) nach Anspruch 8, wobei das Strukturelement (502) einen Körperpanzerungsaufbau
umfasst.
11. Persönliche Körperpanzerungseinheit (600), umfassend eine Keramikplatte (602), ein
massereiches Glied (610) und das auf dem massereichen Glied abgelagerte Schockwellen-Dämpfungsmaterial
nach Anspruch 1.
12. Persönliche Körperpanzerungseinheit (600) nach Anspruch 11, wobei das massereiche
Glied (610) ein Material umfasst, das aus einer Liste von Materialien ausgewählt ist,
bestehend aus: ultrahochmolekularem Polyethylen, einem synthetischen para-Aramid-Faserverbundstoff,
einem Kohlenstofffaserverbundstoff, einem Metall, einem keramischen Werkstoff und
Kombinationen davon.
13. Computer- oder Hardwaregehäuse, umfassend das Schockwellen-Dämpfungsmaterial nach
Anspruch 1.
14. Außenbeschichtung, Folie, Zwischenschicht und/oder -platte, umfassend das Schockwellen-Dämpfungsmaterial
nach Anspruch 1, aufgebracht auf eine vorbestehende Ausrüstung.
15. Fußball-Schienbeinschutz, Brustpolster für Baseball-Fänger, Fußball-Schulterpolster,
Baseballhandschuhe, Golfschläger oder Baseballschläger, umfassend das Schockwellen-Dämpfungsmaterial
nach Anspruch 1.
1. Matériau d'atténuation d'ondes de choc (100), comprenant :
une pluralité de couches d'atténuation de chocs (110), comprenant chacune :
(i) une couche de nanoparticules à gradient (114) contenant une pluralité de nanoparticules
(120) de différents diamètres qui sont disposées selon un gradient ; et
(ii) une couche d'allotropes de carbone (118) disposée de façon adjacente à la couche
de nanoparticules à gradient (114), la couche d'allotropes de carbone (118) contenant
une pluralité d'éléments allotropes de carbone (128) en suspension dans une matrice
(124).
2. Matériau d'atténuation d'ondes de choc selon la revendication 1, dans lequel la couche
de nanoparticules à gradient (114) comprend des nanoparticules (120) d'au moins deux
différents diamètres.
3. Matériau d'atténuation d'ondes de choc selon la revendication 1, dans lequel les éléments
allotropes de carbone (128) sont sélectionnés parmi une liste d'allotropes de carbone
constituée de feuilles de graphène, de nanotubes de carbone, de fullerènes, de feuilles
de graphène fonctionnalisé, de nanotubes de carbone fonctionnalisé, de fullerènes
fonctionnalisés, et de combinaisons de ceux-ci.
4. Matériau d'atténuation d'ondes de choc selon la revendication 1, comprenant en outre
une couche de substrat (104), dans lequel la pluralité de couches d'atténuation de
chocs (110) est disposée sur la couche de substrat (104).
5. Matériau d'atténuation d'ondes de choc selon la revendication 1, dans lequel le gradient
comprend la pluralité de nanoparticules (120) de différents diamètres disposées en
un ensemble à gradient du plus petit diamètre au plus grand diamètre.
6. Casque (400) ou doublure de casque comprenant le matériau d'atténuation d'ondes de
choc selon la revendication 1.
7. Casque (400) selon la revendication 6, comprenant en outre un matériau sélectionné
dans le groupe constitué d'un plastique de haute densité, d'un composite, d'une fibre
de verre, d'un composite de fibres synthétiques de para-aramide, d'un vinyle, d'un
composite acrylonitrile-butadiène-styrène, d'un composite acrylique, et d'un métal.
8. Blindage (500) comprenant le matériau d'atténuation d'ondes de choc selon la revendication
1, le blindage (500) comprenant en outre un élément structural (502) et une plaque
de blindage (510).
9. Blindage (500) selon la revendication 8, dans lequel l'élément structural (502) comprend
au moins l'un d'un plafond, d'un plancher ou d'une paroi d'un véhicule.
10. Blindage (500) selon la revendication 8, dans lequel l'élément structural (502) comprend
une construction de vêtement blindé.
11. Blindage pour vêtement blindé (600) comprenant une plaque en céramique (602), un élément
à masse élevée (610), et le matériau d'atténuation d'ondes de choc selon la revendication
1 disposé sur l'élément à masse élevée.
12. Blindage pour vêtement blindé (600) selon la revendication 11, dans lequel l'élément
à masse élevée (610) comprend un matériau sélectionné parmi une liste de matériaux
constituée d'un polyéthylène à ultra-haute masse moléculaire, d'un composite de fibres
synthétiques de para-aramide, d'un composite de fibres de carbone, d'un métal, d'une
céramique, et de combinaisons de ceux-ci.
13. Boîtier d'ordinateur ou de matériel comprenant le matériau d'atténuation d'ondes de
choc selon la revendication 1.
14. Revêtement extérieur, film, couche intermédiaire et/ou panneau comprenant le matériau
d'atténuation d'ondes de choc selon la revendication 1, appliqué(e) sur un équipement
préexistant.
15. Protège-tibia de football, protection thoracique pour receveur de base-ball, épaulière
de football américain, gant de base-ball, club de golf ou batte de baseball comprenant
le matériau d'atténuation d'ondes de choc selon la revendication 1.